Carrier-Based Aircraft Approach Power Compensator System Design Based on L_1 Adaptive Controller
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- 英文论文题名：Carrier-Based Aircraft Approach Power Compensator System Design Based on L_1 Adaptive Controller
- 论文作者：Ke Lu ; Chunsheng Liu ; Shangjing Wu ; Chunhua Li
- 英文论文作者：Ke Lu ; Chunsheng Liu ; Shangjing Wu ; Chunhua Li ; Science & Technology on Rotorcraft Aeromechanics Laboratory ; China Helicopter Research and Development Institute ; College of Automation Engineering Nanjing University of Aeronautics and Astronautics
- 年：2017
- 作者机构：Science & Technology on Rotorcraft Aeromechanics Laboratory,China Helicopter Research and Development Institute;College of Automation Engineering Nanjing University of Aeronautics and Astronautics;
- 英文论文关键词：Approach Power Compensator System(APCS) ; Dynamic Inversion ; L_1 Adaptive Controller
- 会议召开时间：2017-07-26
- 会议录名称：第36届中国控制会议论文集（A）
- 英文会议录名称：Proceedings of the 36th Chinese Control Conference（A）
- 语种：英文
- 分类号：V271.492
- 学会代码：KZLL
- 会议名称：第36届中国控制会议
- 会议地点：中国辽宁大连
- 主办单位：中国自动化学会控制理论专业委员会
- 学会名称：中国自动化学会控制理论专业委员会
- 页数：4
- 文件大小：139k
- 原文格式：D
- 会议级别：全国
摘要
In this paper,we present a Carrier-Based Aircraft Approach Power Compensator System based on L_1 adaptive controller.A nonlinear dynamic inversion controller serves as the baseline controller for this architecture as command inputs.Then the baseline controller is augmented with an L_1 adaptive controller to cancel out the uncertainties.The main advantage of the new approach is its ability of fast adaptation that leads to uniform transient performance for the system's signals,both inputs and outputs,simultaneously,with guaranteed performance specifications.Simulation results verify the benefit of this new approach.
In this paper,we present a Carrier-Based Aircraft Approach Power Compensator System based on L_1 adaptive controller.A nonlinear dynamic inversion controller serves as the baseline controller for this architecture as command inputs.Then the baseline controller is augmented with an L_1 adaptive controller to cancel out the uncertainties.The main advantage of the new approach is its ability of fast adaptation that leads to uniform transient performance for the system's signals,both inputs and outputs,simultaneously,with guaranteed performance specifications.Simulation results verify the benefit of this new approach.
In this paper,we present a Carrier-Based Aircraft Approach Power Compensator System based on L_1 adaptive controller.A nonlinear dynamic inversion controller serves as the baseline controller for this architecture as command inputs.Then the baseline controller is augmented with an L_1 adaptive controller to cancel out the uncertainties.The main advantage of the new approach is its ability of fast adaptation that leads to uniform transient performance for the system's signals,both inputs and outputs,simultaneously,with guaranteed performance specifications.Simulation results verify the benefit of this new approach.
引文
[1]Fan Ye,Research on Instrument carrier landing system.Nan Jing:Nanjing University of Aeronautics and Astronautics,2008.
[2]Qidan Zhu,Design of Approach Power Compensation System for Carrier-based Aircraft Using Conditional Integral Sliding Surface,in Proceedings of the IEEE International Conference on Information and Automation,2012:821-826.
[3]Shijun Dai,Design of flight/thrust integrated control system using LMI-based Hinf synthesis,in Journal of Nanjing University of Aeronautics&Astronautics,2002:vol.34,no.4,pp.386-390.
[4]Man Cuifang,Carrier-based Aircraft Approach Power Compensator System Design Based on Fuzzy Logic Techniques,in Journal of Nanjing University of Aeronautics&Astronautics,2010:vol.42,no.5,pp.656-660.
[5]Cao,C,and Hovakimyan,N.,Design and Analysis of a Novel L_1 Adaptive Controller,Part 1:Control Signal and Asymptotic Stability,in Proceedings of American Control Conference,Inst.of Electrical and Electronics Engineers,Piscataway,NJ,2006,pp.3397-3402.
[6]Cao,C,and Hovakimyan,N.,Design and Analysis of a Novel L_1 Adaptive Controller,Part 2:Guaranteed Transient Performance,in Proceedings of American Control Conference,Inst.of Electrical and Electronics Engineers,Piscataway,NJ,2006,pp.3403-3408.
[7]Jean-Baptiste Pomet,Laurent Praly,Adaptive nonlinear regulation:estimation from the Lyapunov equation,in IEEE Transactions on Automatic Control,1992:vol.37,no.6,pp.729-740.
[2]Qidan Zhu,Design of Approach Power Compensation System for Carrier-based Aircraft Using Conditional Integral Sliding Surface,in Proceedings of the IEEE International Conference on Information and Automation,2012:821-826.
[3]Shijun Dai,Design of flight/thrust integrated control system using LMI-based Hinf synthesis,in Journal of Nanjing University of Aeronautics&Astronautics,2002:vol.34,no.4,pp.386-390.
[4]Man Cuifang,Carrier-based Aircraft Approach Power Compensator System Design Based on Fuzzy Logic Techniques,in Journal of Nanjing University of Aeronautics&Astronautics,2010:vol.42,no.5,pp.656-660.
[5]Cao,C,and Hovakimyan,N.,Design and Analysis of a Novel L_1 Adaptive Controller,Part 1:Control Signal and Asymptotic Stability,in Proceedings of American Control Conference,Inst.of Electrical and Electronics Engineers,Piscataway,NJ,2006,pp.3397-3402.
[6]Cao,C,and Hovakimyan,N.,Design and Analysis of a Novel L_1 Adaptive Controller,Part 2:Guaranteed Transient Performance,in Proceedings of American Control Conference,Inst.of Electrical and Electronics Engineers,Piscataway,NJ,2006,pp.3403-3408.
[7]Jean-Baptiste Pomet,Laurent Praly,Adaptive nonlinear regulation:estimation from the Lyapunov equation,in IEEE Transactions on Automatic Control,1992:vol.37,no.6,pp.729-740.